IP Library Granted Patent US 7,255,260
Granted Patent B2
US 7,255,260 · App. 10/803,957 · Granted Aug 14, 2007

Assembly for the manufacture of a hollow mechanical part by diffusion bonding and superplastic forming, use of such an assembly and process for manufacturing such a mechanical part

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Quick Facts
Patent No.
US 7,255,260
App. No.
10/803,957
Granted
Aug 14, 2007
Kind
B2
Abstract

A method for manufacturing an assembly including a stack of at least two primary parts, the primary parts being joined together around their periphery with the exception of a place forming a passage so as to define between the two of them a cavity, and the primary parts having, facing the cavity, at least one face that is covered, in a pattern, with a stop-off product containing a binder that can be thermally degraded, and a sealed reservoir having an open end, the end being joined in a sealed manner to the passage in the stack so as to allow communication between the internal space of the reservoir and the cavity, the reservoir being placed under a partial vacuum, this being produced so as to be non-deformable at the temperature and at the pressure at which the diffusion bonding of the said stack takes place.

Claims (21)

1. A process for manufacturing a hollow mechanical part by diffusion bonding and superplastic forming, comprising:

a) providing at least two primary parts, said two primary parts having two faces and a periphery;

b) depositing a stop-off product in a predefined pattern on at least one face among each pair of those faces of the primary parts that are intended to face each other;

c) providing a reservoir having only one open end, the reservoir being produced so as to be non-deformable at the temperature and pressure at which the material of the primary parts undergoes diffusion bonding;

d) joining said primary parts together around their periphery with the exception of a place forming a passage, the primary parts forming a stack and defining, pairwise between them, a cavity that communicates with the passage;

e) placing the stack and the reservoir in a chamber under a partial vacuum of the chamber, thereby the internal volume of said reservoir is placed under a partial vacuum;

f) making a sealed join between the open end of said reservoir and the passage of the stack in the chamber under partial vacuum, so as to form an assembly allowing communication between the internal space of the reservoir and the cavity;

g) heating said chamber to the thermal degradation temperature of the binder, thereby allowing the gases resulting from the degradation of the binder to be sucked into the reservoir;

h) heating said chamber to the diffusion bonding temperature and pressurized to the diffusion bonding pressure, which causes said stack to undergo hot isostatic pressing diffusion bonding;

i) separating said reservoir from the bonded stack;

j) placing the bonded stack in a mould; and

k) bringing the mould to the superplastic forming temperature and an inert gas is injected under the superplastic forming pressure via the passage in the cavity, whereby the stack undergoes inflation and superplastic forming, allowing a blank of the mechanical part to be obtained.

2. The manufacturing process according to claim 1 , wherein said joining the primary parts and the making the sealed join are carried out by electron beam welding.

3. The manufacturing process according to claim 1 , wherein said partial vacuum is between 0.01 and 0.1 Pa.

4. The manufacturing process according to claim 1 , wherein said mechanical part is a hollow turbomachine blade, in particular a fan rotor blade, and wherein the stack comprises three primary parts that are made up of a suction side primary part, a central plate and a pressure side primary part.

5. The manufacturing process according to claim 1 , wherein the providing a reservoir includes providing a reservoir configured to withstand a temperature of at least 900° C. and a pressure of at least 4×10 6 Pa.

6. The manufacturing process according to claim 1 , wherein the providing a reservoir includes providing a reservoir made from a nickel-based or cobalt-based metal alloy.

7. The manufacturing process according to claim 1 , wherein the providing a reservoir includes providing a reservoir with a volume between 10 and 100 times a volume of the cavity in the stack.

8. The manufacturing process according to claim 1 , wherein the heating said chamber to the diffusion bonding temperature includes heating said chamber to the diffusion bonding temperature between 200° C. and 400° C.

9. The manufacturing process according to claim 3 , wherein the placing the stack and the reservoir in a chamber under a partial vacuum of the chamber includes placing the stack and the reservoir in a chamber under a partial vacuum of 0.03 to 0.07 Pa.

10. The manufacturing process according to claim 9 , wherein the placing the stack and the reservoir in a chamber under a partial vacuum of the chamber includes placing the stack and the reservoir in a chamber under a partial vacuum of 0.05 Pa.

Assignments (4)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
CHANGE OF NAME Recorded Feb 20, 2008
From: SNECMA MOTEURS
To: SNECMA
Reel/Frame 020609/0569 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 28, 2004
From: FRANCHET, JEAN-MICHEL; GESMIER, PATRICK
To: SNECMA MOTEURS
Reel/Frame 015627/0698 →